Three-dimensional interactions between an advecting vortex tube and a vapor
izing droplet, described by the Navier-Stokes, energy, and species equation
s, cause fluctuations in the droplet heating and vaporization, manifested b
y temporal and time-averaged variations in the droplet Nusselt and Sherwood
numbers. Stefan flux not only inhibits the droplet heating, it also 'block
s' the influence of vortex collision on the droplet interface inhibiting Nu
sselt number perturbations. The Stefan flux has a primary effect on the Nus
selt number and a secondary one on the Sherwood number. Fluctuations in She
rwood number can be significant in magnitude and exhibit self-similarity in
both the temporal and time-averaged response. Derived correlations are dem
onstrated to be valid for at least three common fuel droplets (n-heptane, n
-octane, n-decane). Furthermore, they quantify the effect of vortex collisi
on on the droplet vaporization and compliment the accepted correlations for
droplets in axisymmetric hows. It follows that, in spray combustion system
s, vortical structures could significantly affect transport mechanisms, vap
orization rates, and local mixture ratios. (C) 2000 Elsevier Science Ltd. A
ll rights reserved.